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Aerodynamic performance of several passive vortex generator configurations on an Ahmed body subjected to yaw angles

机译：几种被动涡流发生器配置的空气动力学性能对偏航角度的艾哈迈德机身上的配置

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H. Viswanathan;
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1. Experimental study on Ahmed's body drag coefficient for different yaw angles [J] . Bello-Millan F. J., Makela T., Parras L., Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2016,第Null期

机译：不同偏航角下艾哈迈德身体阻力系数的实验研究
2. Prediction of the aerodynamic loads on a railway train in a cross-wind at large yaw angles using an integrated two- and three-dimensional source/vortex panel method [J] . T. W. Chiu Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 1995,第1期

机译：使用集成的二维和三维源/涡旋面板方法预测大偏航角下侧风中火车上的空气动力负荷
3. Prediction of the aerodynamic loads on a railway train in a cross-wind at large yaw angles using an integrated two- and three-dimensional source/vortex panel method [J] . T. W. Chiu Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 1995,第1期

机译：使用集成的二维和三维源/涡旋面板方法预测大偏航角下侧风中火车上的空气动力负荷
4. Effects of Tunable Angle for Vortex Generators on Aerodynamic Performances of Airfoils [C] . Hu Yu, Bintang Yang, Xiaoqing Sun, International Conference on Applied Engineering, Materials and Mechanics . 2017

机译：可调谐角度对涡流发生器对翼型空气动力学性能的影响
5. Effect of Boundary Layer Thickness and Passive Vortex Generators on the Wake of a Blunt Trailing Edge Profiled Body [D] . Zhao, Wenyi. 2017

机译：边界层厚度和无源涡流发生器对钝后缘轮廓物体的尾迹的影响
6. Vortex wake downwash distribution aerodynamic performance and wingbeat kinematics in slow-flying pied flycatchers [O] . Florian T. Muijres, Melissa S. Bowlin, L. Christoffer Johansson, 2012

机译：慢速飞行捕蝇器的涡流尾流下冲分布空气动力性能和机翼运动学
7. Experimental and Computational Analysis on Aerodynamic Behavior of a Car Model with Vortex Generators at Different Yaw Angles [O] . G. Shankar, G. Devaradjane 2018

机译：不同偏航角的涡流发生器汽车模型空气动力学行为的实验和计算分析
8. Prediction of Normal Force, Pitching Moment,and Yawing Force on Bodies of Revolution at Angles of Attack up to 50Degrees Using a Concentrated Vortex Flow-Field Model. [R] . wardlaw,andrew b. jr 1974

机译：利用集中涡流场模型预测50度攻角下旋转体的法向力，俯仰力和偏航力。

Aerodynamic performance of several passive vortex generator configurations on an Ahmed body subjected to yaw angles

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